Numerical study of nozzle scale effect upon high-pressure oxygen-iodine laser performance
2001
The numerical calculations of the gain and dissociation degree of molecular iodine in a supersonic COIL channel are reported for supersonic mixing of flows and 0.2-, 0.3-, 0.4- mm- height critical sections of nozzles profiled for Mach number 2.5 to 4.0.
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